Bringerofpain
27-06-2004, 14:09
*note, Huge orders will ususally take 2- 6 real days depending on the order. *
GROUND SYSTEMS
M60 PATTON
http://www.globalsecurity.org/military/systems/ground/images/m-60a1-dvic351-s.jpg
Weight 60 tons Length 32'4" Width 13'6" Height 12'6" Ground Clearance 18in Track Width 28in Forward speed 30 mph Reverse speed 10 mph Engine 750 hp Continental AVDS-1790 V-12 diesel Vertical obstacle climb 49 in Maximum width ditch 108 in Fording Depth 48 in Main Gun 105mm/51cal M68 rifiled gun with 63 rounds Coaxial machinegun M240 - 7.62mm with 5,950 rounds Commander's machinegun M85 - .50 cal antiaircraft gun with 900 rounds Sensors and Fire Control M21 solid state along ballistic computer, AN/VVG-2 ruby laser rangefinder usable by both commander and gunner, AN/vsg-2 Tank thermal Sights (TTS) withlaser rangerfinder and Mercury-Cadmium-Telluride (HgCdTe) IR detector for passive night and dust vision.
price:2million
M113 ARMED PERSONNEL CARRIER
http://www.globalsecurity.org/military/systems/ground/images/m113-001-s.jpg
Length 191.5" Width 105.75" Height 86.5" Clearance 16" Weight, combat loaded 27,180 lb. (12,329 kg) Maximum weight 31,000 lb. (14,061 kg) Net weight 23,880 lb. (10,832 kg) Air drop weight 22,128 lb. (10,037 kg) Personnel capacity 2 + 11 Fuel tank capacity 95 gallons (360 liters) Ground pressure 8.63 psi (0.60 kg/cm2)
Performance
Speed on land 41 mi/h (66 km/h) Speed in water, with track 3.6 mi/h (5.8 km/h) Cruising range 300 mi (483 km) Turning radius Pivot to infinite Slope 60% Side slope 40% Trench crossing 66 in. (168 cm) Vertical wall climbing 24 in. (61 cm) Braking (20-0 mi/h) 40 ft.
Engine
Make and model Detroit Diesel 6V53T Displacement 318 in.3 (5.2 liter) Fuel Diesel (DF2) Rated horsepower 275 hp Gross horsepower-to-weight ratio 20.2 hp/ton
Transmission, Automatic
Make and model Allison X200-4B Type Hydrokinetic Steering Hydrostatic Brake type Multiple wet plate
Running Gear
Suspension Torsion bar Road wheels 5 per side, 24 inch diameter (61 cm) Track type Steel single pin, detachable rubber pad Number of shoes 63 left, 64 right Track pitch 6 in. (15.2 cm) Track width 15 in. (38 cm) Shock absorbers 3 per side Wheel travel 9.0 in. (22.9 cm)
Electrical System
Generator Amperes 200, 300 optional Volts, dc 28 Batteries 4, type 6TL, 120 amp-hr, 12-volt each
Armament
50 cal MG 2,000 ready rds.
Armor
Basic hull 5083 Aluminum Bolt-on armor kit Steel armor Mine armor Steel armor Gun shield kit Steel armor Spall suppressant Composite panel
Fire Extinguishers
Fixed 5 lb. (2.3 kg) CO2 for engine compartment Portable 5 lb. (2.3 kg) CO2
price:3million
XM104 WOLVERINE( heavy assault bridge system)
http://www.globalsecurity.org/military/systems/ground/images/wol3-s.jpg
http://www.globalsecurity.org/military/systems/ground/images/wolverine2-s.jpg
Crew 2 Soldiers (12B MOS) Weight 68.7 TONS Powerpack AGT-1500 Turbine X1100 Trans Launch Power Unit Integrated APU Powers Launcher Silent Watch Fire Protection Automatic 3 Zone Extinguisher System Electrical System 24 Volts Tread 112.0 in. Track Width 25.0 in. Vertical Obstacle 36.7 in. Trench Crossing 106 in. Ground Clearance 19.0 in. Fording 48 in. (w/o kit) Speed Cross Country: 32.2 kph Improved Roads: 56 kph Maximum:45 MPH (Governed) Cruising Range 260 Miles Heavy Assault Bridge System Gap Crossing Length 24.0 M (26 Meter Length) Mission Load Class [MLC] 70.0 TONS Crossing Speed 13-16 kph Durability 5000 MLC70 Crossings Launch Time Less than 5 min. Recovery Time 10 Minutes (5 Min. to Engage, 5 Min to store in Travel Mode
price: 3.5million
M55 8" SELF PROPELLED HOWITZER(T108)
http://www.globalsecurity.org/military/systems/ground/images/m55-img17-s.jpg
M55: General Manufacturer Pacific Car and Foundry Co. . M55: Dimensions Combat weight 98,000lbs / 44,000kg Length without howitzer 311" / 790cm Height 140"360cm Width Howitzer overhang forward 0" . M55: Armament Type 8" Howitzer M47 Mount T58 in turret Ammunition 10 rounds Traverse 60° (30° left or right) Elevation +65° to -5° rate of fire one round every two minutes maximum range 16,900 meters Type .50cal M2HB MG Mount Flexible in turret AA mount Ammunition Traverse 360° (manual) Elevation Manual . M55: Armor Assembly Welding Maximum .59"1.5cm Hull Rolled homogeneous steel Turret Rolled homogeneous steel . M55: Automotive Engine Continental AV-1790-5B; 12 cylinder, 4 cycle, 90° vee gasoline Horsepower Gross: 810@2800rpm Transmission Allison CD-850-4A, two ranges forward, 1 reverse Steering Wobble stick Brakes Multiple disc . M55: Suspension Type Torsion bar Road wheels 7 independently sprung dual/track Track return rollers 3 dual/track Drive sprockets 11-tooth front drive Idlers Rear road wheels serve as adjustable trailing idlers M55: Track Type T84E1 Center guide, double pin, chevron, rubber Width 23"58cm Pitch 6"15cm . M55: Performance Max level road speed 32mph51kph Max grade 0.6 Min turning diameter Pivot Cruising range ~160mi, roads~260km, roads Max trench 90"230cm Max vertical obstacle 40"100cm Max fording depth 48"120cm
price: 3million
* AIR UNITS*
T-28 TALON
http://www.globalsecurity.org/military/systems/aircraft/images/t-38-199905172ship-s.jpg
Primary Function Advanced jet pilot trainer
Builder Northrop Corp.
Power Plant Two General Electric J85-GE-5 turbojet engines with afterburners
Thrust 2,900 pounds (1,315 kilograms) with afterburners
Length 46 feet, 4 1/2 inches (14 meters)
Height 12 feet, 10 1/2 inches (3.8 meters)
Wingspan 25 feet, 3 inches (7.6 meters)
Speed 812 mph (Mach 1.08 at sea level)
Ceiling Above 55,000 feet (16,667 meters)
Maximum Takeoff Weight 12,500 pounds (5,670 kilograms)
Range 1,000 miles (870 nautical miles)
Armament T-38A: none; AT-38B has provisions for external armament
Unit Cost $756,000
F-14 TOMCAT
http://www.globalsecurity.org/military/systems/aircraft/images/f-14-dvic222-s.jpg
Function Carrier-based multi-role strike fighter
Contractor Grumman Aerospace Corporation
Propulsion F-14: two Pratt & Whitney TF-30P-414A
turbofan engines with afterburners;
F-14B and F-14D: two General Electric F-110-GE-400
augmented turbofan engines with afterburners
Thrust F-14A: 20,900 pounds (9,405 kg) static thrust per engine;
F-14B and F-14D: 27,000 pounds (12,150 kg) per engine Length 61 feet 9 inches (18.6 meters) Height 16 feet (4.8 meters) Basic Weight approx 43,600 pounds Maximum Takeoff Weight 72,900 pounds (32,805 kg) Wingspan 64 feet (19 meters) unswept,
38 feet (11.4 meters) swept Reference wing area 565 sq ft. Wing aspect ratio 7.28 Ceiling Above 53,000 feet Max G 6.5 Speed 1,584 mph (2,548km/h) Max. speed at 40,000 ft (12,200 m)
Max Mach Number = 1.88
Cruise Mach Number = .72
Carrier Approach Speed = 125 kts Fuel 16, 200 lbs. Internal fuel
3, 800 lbs. External fuel Maximum range 1,600 nm (2,573km) Mission Radius 500 nm (930 km) Hi-Med-Hi strike profile
380 nm (700 km) Hi-Lo-Lo-Hi strike profile Airfield 2,500 ft. Field takeoff distance
2,400 ft. Field landing distance Crew Two: pilot and radar intercept officer
Armament Up to 13,000 pounds of
Air-to-Air Missiles (up to)
6 AIM-7 Sparrows <../munitions/aim-7.htm>
4 AIM-9 Sidewinder <../munitions/aim-9.htm>
6 AIM-54 Phoenix <../munitions/aim-54.htm>
air-to-ground ordnance
MK-82 <../munitions/mk82.htm> (500 lbs.)
4 MK-83 <../munitions/mk83.htm>(1,000 lbs.)
4 MK-84 <../munitions/mk84.htm> (2,000 lbs.)
MK-20 <../munitions/mk20.htm> cluster bomb
4 GBU-10 <../munitions/gbu-10.htm> LGB
GBU-12 MK-82 <../munitions/gbu-12.htm>LGB
4 GBU-16 MK-83 <../munitions/gbu-16.htm>LGB
4 GBU-24 MK-84 <../munitions/gbu-24.htm>LGB
4 GBU-31 <../munitions/gbu-31.htm> JDAM <../munitions/jdam.htm>(2,000 lbs)
one MK-61A1 Vulcan 20mm cannon
Selected F-14A and B are wired to carry TARPS <../../../../irp/program/collect/tarps.htm>
All F-14D's are wired to carry the TARPS <../../../../irp/program/collect/tarps.htm>
Countermeasures AN/ALR-45 radar warning receiver [Itek] AN/ALR-67 radar warning receiver [F-14D] AN/ALQ-167 ECM Pod [F-14D] AN/ALE-50 towed decoy [F-14D] Date Deployed First flight: December 21st 1970 Inventory 157 F-14A/B
53 F-14D
Phasing out one squadron / year
All to be withdrawn by 2010
F-14 orginally designed for 6,000 flight hours
Currently certified for 7,350 flight hours
Potential for extension to 8,000 or 9,000 flight hours
Price:38 million
FH-1 PHANTOM
First flight Jan. 26, 1945
Wingspan 40 feet 9 inches (wings folded, 16 feet, 3 inches)
Length 38 feet 9 inches
Height 14 feet, 2 inches
Weight 10,035 lbs
Speed 500 mph (max.)
Ceiling 41,100 ft
Range 695 miles
Accommodation One crew
Armament Four 22 mm cannons
Power plant Two 1,600-pound thrust Westinghouse J30-WE-20 turbojets
Price:12million
F-16XL FIGHTING FALCON
http://www.globalsecurity.org/military/systems/aircraft/images/f-16-eglin1-s.jpg
Crew size F-16XL-2 two-seat cockpit
F-16XL-1 single-seat aircraft
Length 54.2 ft (16.52 m)
Wingspan 34.3 ft (10.45 m)
height at vertical tail 17.7 ft (5.39 m).
Max. weight 48,000 lb (17,915.60 kg)
Engines F-16XL-2 General Electric F110-GE-129 engine (with afterburner) rated at 29,000 lb thrust.
F-16XL-1 Pratt and Whitney 100-PW-100 engine (with afterburner), rated at 23,830 lb thrust.
Controls Both aircraft featured an analog fly-by-wire electronic flight control system during the laminar flow research. The single-seat aircraft now has a digital flight control system.
Wing construction The delta (cranked arrow) wings on both aircraft are manufactured of advanced graphite composites to provide strength for high wing loads during flight.
Design load Baseline F-16XL: 9 "Gs".
Modified F-16XL: 3 "Gs")
Maximum Speed F-16XL-2, Mach 2 (approx. 1,400 mph) (2,253 k/hr)
F-16XL-1, Mach 1.8 (approx. 1,260 mph)
Range Over 2,500 nautical miles (4,630 k), without in-flight refueling, and unlimited with in-flight refueling
Price: 40 million
F-22 RAPTOR
http://www.globalsecurity.org/military/systems/aircraft/images/f-22-9733679-s.jpg
Official Nickname Raptor
User U. S. Air Force
Function Air superiority fighter
Contractors Lockheed Martin Aeronautical Systems: F-22 program management, the integrated forebody (nose section) and forward fuselage (including the cockpit and inlets), leading edges of the wings, the fins and stabilators, flaps, ailerons, landing gear and final assembly of the aircraft.
Lockheed Martin Tactical Aircraft Systems: Center fuselage, stores management, integrated navigation and electronic warfare systems (INEWS), the communications, navigation, and identification (CNI) system, and the weapon support system.
Boeing: wings, aft fuselage (including the structures necessary for engine and nozzle installation), radar system development and testing, avionics integration, the training system, and flight-test development and management.
Pratt & Whitney: F119-PW-100 engines that power the Raptor.
Major Subcontractors Approximately 240 firms in 37 states are considered major subcontractors
More than 1,150 firms in 46 states and Puerto Rico, along with firms in seven international countries make up the F-22/F119 subcontractor team.
(partial list):
Northrop Grumman
Texas Instruments
Kidde-Graviner Ltd.
Allied-Signal Aerospace
Hughes Radar Systems
Harris
Fairchild Defense
GEC Avionics
Lockheed Sanders
Kaiser Electronics
Digital Equipment Corp.
Rosemount Aerospace
Curtiss-Wright Flight Systems
Dowty Decoto, EDO Corp.
Lear Astronics Corp.
Parker-Hannifin Corp.
Simmonds Precision
Sterer Engineering
TRW
XAR
Motorola
Hamilton Standard
Sanders/GE Joint Venture
Menasco Aerospace
Projected Employment 15,000 in EMD and 27,000 in production
Propulsion two Pratt & Whitney F119-PW-100 engines
Thrust 35,000 lbst
Length 62.08 feet, 18.90 meters
Height 16.67 feet, 5.08 meters
Wingspan 44.5 feet, 13.56 meters
Wing Area 840 square feet
Horizontal Tailspan 29 feet, 8.84 meters
Maximum Takeoff Weight
Ceiling
Speed Mach 1.8 (supercruise: Mach 1.5)
Crew one pilot
Armament Two AIM-9 Sidewinders
six AIM-120C Advanced Medium-Range Air-to-Air Missiles (AMRAAM)
one 20mm Gatling gun
two 1,000-pound Joint Direct Attack Munitions (JDAM)
First flight: September 7, 1997
Flight Test Aircraft: Nine
Flight Test Program Length 1997 until 2003 (Approximately 2,700 flights covering roughly 4,800 test hours in EMD)
Price: 45million
B-52 STRATOFORTRESS( note, if you are less than a month old, you will be sold the ones without nuclear capability.)
http://www.globalsecurity.org/wmd/systems/images/b52-bomb-s.jpg
Primary Function: Heavy bomber
Contractor: Boeing Military Airplane Co.
Power Plant: Eight Pratt & Whitney engines TF33-P-3/103 turbofan
Thrust: Each engine up to 17,000 pounds (7,650 kilograms)
Length: 159 feet, 4 inches (48.5 meters)
Height: 40 feet, 8 inches (12.4 meters)
Wingspan: 185 feet (56.4 meters)
Speed: 650 miles per hour (Mach 0.86)
Ceiling: 50,000 feet (15,151.5 meters)
Weight: Approximately 185,000 pounds empty (83,250 kilograms)
Maximum Takeoff Weight: 488,000 pounds (219,600 kilograms)
Range: Unrefueled 8,800 miles (7,652 nautical miles)
Armament:
NOTE: The B-52 can carry 27 internal weapons. Authoritative sources diverge as to maximum munition loads, with some suggesting as many as 51 smaller munitions and 30 larger munitions, while others suggest maximum loads of 45 and 24, respectively.
The Heavy Stores Adaptor Beam [HSAB] external pylon can carry only 9 weapons which limits the total carry to 45 (18 external).
The AGM-28 pylon could carry lighter weapons like the MK-82 and can carry 12 weapons on each pylon, for a total of 24 external weapons, for a the total of 51. However, the AGM-28 pylon is no longer used, so the B-52 currently carries on HSABs, limiting the external load to 18 bombs, or a total of 45 bombs.
Approximately 70,000 pounds (31,500 kilograms) mixed ordnance -- bombs, mines and missiles.
NUCLEAR
20 ALCM
12 SRAM [ext]
12 ACM [ext]
2 B53 [int]
8 B-61 Mod11 [int]
8 B-83 [int]
CONVENTIONAL
51 CBU-52 (27 int, 18 ext)
51 CBU-58 (27 int, 18 ext)
51 CBU-71 (27 int, 18 ext)
30 CBU 87 (6 int, 18 ext)
30 CBU 89 (6 int, 18 ext)
30 CBU 97 (6 int, 18 ext)
51 M117
18 Mk 20 (ext)
51 Mk 36
8 Mk 41
12 Mk 52
8 Mk 55
8 Mk 56
51 Mk 59
8 Mk 60 (CapTor)
51 Mk. 62
8 Mk. 64
8 Mk 65
51 MK 82
18 MK 84 (ext)
PRECISION
18 JDAM (12 ext)
30 WCMD (16 ext)
8 AGM-84 Harpoon
20 AGM-86C CALCM
8 AGM-142 Popeye [3 ext]
18 AGM-154 JSOW (12 ext)
12 AGM-158 JASSSM [ext]
12 TSSAM
Systems AN/ALQ-117 PAVE MINT active countermeasures set
AN/ALQ-122 false target generator [Motorola]
AN/ALQ-153 tail warning set [Northrop Grumman]
AN/ALQ-155 jammer Power Management System [Northrop Grumman]
AN/ALQ-172(V)2 electronic countermeasures system [ITT]
AN/ALR-20A Panoramic countermeasures radar warning receiver
AN/ALR-46 digital warning receiver [Litton]
AN/ALT-32 noise jammer
12 AN/ALE-20 infra-red flare dispensers
6 AN/ALE-24 chaff dispensers
AN/ANS-136 Inertial Navigation Set
AN/APN-224 Radar Altimeter
AN/ASN-134 Heading Reference
AN/APQ-156 Strategic Radar
AN/ASQ-175 Control Display Set
AN/AYK-17 Digital Data Display
AN/AYQ-10 Ballistics Computer
AN/AAQ-6 FLIR Electro-optical viewing system
AN/AVQ-22 Low-light TV Electro-optical viewing system
AN/ARC-210 VHF/UHF communications
AN/ARC-310 HF radio communications
CRM-114 Discriminator
Crew: Five (aircraft commander, pilot, radar navigator, navigator and electronic warfare officer)
Accommodations: Six ejection seats
Unit Cost: $30 million
B-1B LANCER
http://www.globalsecurity.org/wmd/systems/images/b1_cbus-s.jpg
Primary Function: Long-range, multi-role, heavy bomber
Builder: Rockwell International, North American Aircraft
Operations Air Frame and Integration: Offensive avionics, Boeing Military Airplane; defensive avionics, AIL Division
Power Plant: Four General Electric F-101-GE-102 turbofan engine with afterburner
Thrust: 30,000-plus pounds (13,500-plus kilograms) with afterburner, per engine
Length: 146 feet (44.5 meters)
Wingspan: 137 feet (41.8 meters) extended forward,
79 feet (24.1 meters) swept aft
Height: 34 feet (10.4 meters)
Weight: Empty, approximately 190,000 pounds (86,183 kilograms)
Maximum Takeoff Weight: 477,000 pounds (214,650 kilograms)
Speed: 600+ mph (Mach .92) @ 500 feet
825 mph (Mach 1.25) @ 50,000 feet
Rotate and Takeoff Speeds: 210 Gross - 119 Rotate kts / 134 kts Takeoff
390 Gross - 168 kts Rotate / 183 kts Takeoff
Landing Speeds: 210 Gross - 145 kts
380 Gross - 195 kts
Range: 7,455 miles, unrefueled
3,444 miles with normal weapons load
Ceiling: 60,000 feet (18,000 meters)
Crew: Four (aircraft commander, pilot, offensive systems officer and defensive systems officer)
Armament: NUCLEAR
CONVENTIONAL
84 Mk 62
84 MK82
30 CBU 87
30 CBU 89
30 CBU 97
12 Mk 65
PRECISION
30 WCMD
24 JDAM
12 GBU-27
12 AGM-154 JSOW
12 TSSAM
Date Deployed: June 1985
Cost: $200 million
B-2 SPIRIT (note, if you are under a month old, have enough money, and wish to purchase one of these, you will recieve the plane without nuclear capabilities)
http://www.globalsecurity.org/wmd/systems/images/b2bombs_s.jpg
http://www.globalsecurity.org/wmd/systems/images/b-2-clouds-s.jpg
Primary function: Multi-role heavy bomber.
Prime Contractor: Northrop Grumman Corp.
Contractor Team: Boeing Military Airplanes Co.,
General Electric Aircraft Engine Group
Hughes Training Inc., Link Division
Power Plant/Manufacturer: Four General Electric F-118-GE-100 engines
Thrust: 17,300 pounds each engine (7,847 kilograms)
Length: 69 feet (20.9 meters)
Height: 17 feet (5.1 meters)
Wingspan: 172 feet (52.12 meters)
Speed: High subsonic
Ceiling: 50,000 feet (15,152 meters)
Takeoff Weight (Typical): 336,500 pounds (152,635 kilograms)
Range: Intercontinental, unrefueled
Armament: NUCLEAR
16 B61
16 B83
16 AGM-129 ACM
16 AGM-131 SRAM 2 CONVENTIONAL
80 MK82 [500lb]
16 MK84 [2000lb]
34-36 CBU87
34-36 CBU89
34-36 CBU97
PRECISION
80 GBU-30 JDAM [500lb]
16 GBU-32 JDAM [2000lb]
8 GBU 27
8 EGBU 28
8 GBU 36
8 GBU 37
8-16 AGM-154 JSOW
8-16 AGM-137 TSSAM
Payload: 40,000 pounds (18,000 kilograms)
Crew: Two pilots
Unit cost: Approximately $2.1 billion [average]
AH-64 APACHE
http://www.globalsecurity.org/military/systems/aircraft/images/apache_hellfire-s.jpg
http://www.globalsecurity.org/military/systems/aircraft/images/ah-64-dvic292-s.jpg
Contractors Boeing McDonnell Douglas Helicopter Systems(Mesa, AZ)
General Electric (Lynn, MA)
Martin Marietta (Orlando, FL) Propulsion Two T700-GE-701Cs Crew Two AH-64A AH-64D Length 58.17 ft (17.73 m) 58.17 ft (17.73 m) Height 15.24 ft (4.64 m) 13.30 ft (4.05 m) Wing Span 17.15 ft (5.227 m) 17.15 ft (5.227 m) Primary Mission Gross Weight 15,075 lb (6838 kg)
11,800 pounds Empty 16,027 lb (7270 kg) Lot 1 Weight Hover In-Ground Effect (MRP) 15,895 ft (4845 m)
[Standard Day]
14,845 ft (4525 m)
[Hot Day ISA + 15C] 14,650 ft (4465 m)
[Standard Day]
13,350 ft (4068 m)
[Hot Day ISA + 15 C] Hover Out-of-Ground Effect (MRP) 12,685 ft (3866 m)
[Sea Level Standard Day]
11,215 ft (3418 m)
[Hot Day 2000 ft 70 F (21 C)] 10,520 ft (3206 m)
[Standard Day]
9,050 ft (2759 m)
[Hot Day ISA + 15 C] Vertical Rate of Climb (MRP) 2,175 fpm (663 mpm)
[Sea Level Standard Day]
2,050 fpm (625 mpm)
[Hot Day 2000 ft 70 F (21 C)] 1,775 fpm (541 mpm)
[Sea Level Standard Day]
1,595 fpm (486 mpm)
[Hot Day 2000 ft 70 F (21 C)] Maximum Rate of Climb (IRP) 2,915 fpm (889 mpm)
[Sea Level Standard Day]
2,890 fpm (881 mpm)
[Hot Day 2000 ft 70 F (21 C)] 2,635 fpm (803 mpm)
[Sea Level Standard Day]
2,600 fpm (793 mpm)
[Hot Day 2000 ft 70 F (21 C)] Maximum Level Flight Speed 150 kt (279 kph)
[Sea Level Standard Day]
153 kt (284 kph)
[Hot Day 2000 ft 70 F (21 C)] 147 kt (273 kph)
[Sea Level Standard Day]
149 kt (276 kph)
[Hot Day 2000 ft 70 F (21 C)] Cruise Speed (MCP) 150 kt (279 kph)
[Sea Level Standard Day]
153 kt (284 kph)
[Hot Day 2000 ft 70 F (21 C)] 147 kt (273 kph)
[Sea Level Standard Day]
149 kt (276 kph)
[Hot Day 2000 ft 70 F (21 C)] Range 400 km - internal fuel
1,900 km - internal and external fuel Armament M230 30mm Gun <systems/m230.htm>
70mm (2.75 inch) Hydra-70 Folding-Fin Aerial Rockets <../munitions/hydra-70.htm>
AGM-114 Hellfire <../munitions/agm-114.htm> anti-tank missiles
AGM-122 Sidearm <../munitions/agm-122.htm>anti-radar missile
AIM-9 Sidewinder <../munitions/aim-9.htm>Air-to-Air missiles
<images/ah-64d-mission-image20.jpg> <images/ah-64d-mission-image20.jpg>Mission Equipment Target Acquisition and Designation System /
Pilot Night Vision System Reliability The general objective of aircraft readiness is to achieve 75% Mission Capable.
price:15million
*NAVAL*
BB-61 IOWA-CLASS BATTLESHIP
http://www.globalsecurity.org/military/systems/ship/images/bb-62-8406362-s.jpg
http://www.globalsecurity.org/military/systems/ship/images/missour2-s.jpg
Displacement Light Displacement: 45231 tons
Full Displacement: 57271 tons
Dead Weight: 12040 tons
Length Overall Length: 888 ft
Waterline Length: 860 ft
Beam Extreme Beam: 109 ft
Waterline Beam: 108 ft
Draft Maximum Navigational Draft: 38 ft
Draft Limit: 37 ft
Max Speed 35 knots
Power Plant Eight boilers, four geared turbines, four shafts, 212,000 shaft horsepower
Armament 32 - Tomahawk ASM/LAM - 8 armored box launchers
16 - Harpoon ASM - 4 quad cell launchers
9 - Mk 7 - 16-inch / 50 caliber guns
12 - Mk 28 - 5-inch / 38 caliber guns
4 - Mk 15 - 20mm Phalanx CIWS
Combat Systems SPS-49 Air Search Radar
SPS-67 Surface Search Radar
4 Mk37 Gun Fire Control
2 Mk38 Gun Direction
1 Mk40 Gun Director
1 SPQ-9
SLQ-25 NIXIE
SLQ-32 EW system
Aircraft None embarked
landing area and unhangared parking area
4 SH-3 or
4 SH-60
Compliment 1,515 ship's company
65 officers
1,450 enlisted
58 Marines
Builders New York Navy Yard -- BB 61, 63
Philadelphia Navy Yard -- BB 62, 64
Price: 3billion
[b]CVN-68 NIMITZ-CLASS
http://www.globalsecurity.org/military/systems/ship/images/vinson-bow-s.jpg
Builder Newport News Shipbuilding Co., Newport News, Va.
Power Plant Two Nuclear Power Plant (A4W Pressurized Water Reactor)
Four shafts, Four propellers, with five blades each
Length, overall 1,092 feet (332.85 meters)
Flight Deck Width 252 feet (76.8 meters)
Beam 134 feet (40.84 meters)
Displacement Approx. 97,000 tons (87,300 metric tons) full load
Speed 30+ knots (34.5+ miles per hour)
Aircraft 85
Aircraft elevators Four
Catapults Four
Armament 4 Sea Sparrow launchers
3 Phalanx CIWS 20mm mounts [Nimitz & Ike]
4 Phalanx CIWS 20mm mounts [Vinson and later]
Combat Systems SPS-48E 3-D air search radar
SPS-49(V)5 2-D air search radar
3 Mk91 Fire Control
Multi-Function Radar (MFR) [CVN-77]
Volume Search Radar (VSR) [CVN-77]
AN/SLQ-32(V)4 active jamming/deception
AN/WLR-1H ESM
Service Life 50 years
Crew Ship's Company: 3,200
Air Wing: 2,480
Departments
Administrative
Aircraft Maintenance
Air
Chaplain
Combat Systems
Deck
Dental
Engineering
Legal
Maintenance
Medical
Navigation
Operations
Public Affairs
Reactor
Safety
Supply
Training
Weapons
Price: 4billion
ohio-class SSBN ( note, if you are under 1 month old, you shall be sold the non-nuclear subs)
http://www.globalsecurity.org/wmd/systems/images/ssbn_uw_s.jpg
http://www.globalsecurity.org/wmd/systems/images/ssbn731-p01a_s.jpg
Builders: General Dynamics Electric Boat Division.
Power Plant: One S8G nuclear reactor
core reloaded every nine years
two geared steam turbines,
one shaft, output of 60,000 hp
Length: 560 feet (170.69 meters)
Beam: 42 feet (10.06 meters)
Displacement: Surfaced: 16,764 tons
Submerged:18,750 tons
Speed: Official: 20+ knots (23+ miles per hour, 36.8 +kph)
Actual: 25 knots submerged speed
Operating Depth: Official: "greater than 800 feet"
Actual: greater than 1,000 feet
Armament: 24 - tubes for Trident I and II,
4 - torpedo tubes with Mk48 Torpedoes
Systems: AN/BQQ-6 passive-only spherical bow and conformal sonar arrays
AN/BQR-19 active short range navigation set
AN/BQS-13 Active sonar
AN/BQS-15 high-frequency short range under-ice sonar set
TB-16B or TB-23 passive towed array
AN/BPS-15A I-Band search and navigation radar
AN/WLR-8(V) radar receiver
MK 98 Digital Missile Fire Control System (FCS) for Trident missiles
MK 118 Torpedo FCS
Crew: 15 Officers, 140 Enlisted
Price:500million
SSN-21 SEAWOLF CLASS SUB
http://www.globalsecurity.org/military/systems/ship/images/ssn-21-dvic117-s.jpg
Builders General Dynamics Electric Boat Division
Power Plant One S6W reactor
one shaft at with 52,000 shp with pumpjet propulsor
Improved Performance Machinery Program Phase II one secondary propulsion submerged motor
Length 353 feet (107.6 meters)
Draft 35 feet (10.67 meters)
Beam 40 feet (12.2 meters)
Displacement 7,460 ton surface displacement
9,137 tons submerged displacement
Speed Official: 25+ knots (28+ miles per hour, 46.3+ kph)
Actual: 35 knots maximum submerged speed
Actual: 20 knots tactical ["silent"] speed
Operating Depth Official: "greater than 800 feet"
Actual: About 1600 feet
Jane's Fighting Ships: 2000 feet
Armament eight 660-mm torpedo tubes
50 Tomahawk cruise missiles or
50 Harpoon antiship missiles or
50 Mark 48 ADCAP torpedoes or
up to 100 mines
Systems AN/BSY-2 active-passive Sonar/Fire Control w/
hemispherical bow array and wide aperture array
TB-16B or TB-23 towed array
AN/BPS-16 search and navigation radar
AN/WLQ-4(V)1 ES receiver
Central Combat System (CCS) MK2
Link 11 Tactical data link
OTCIXS Tactical data link
Crew 12 Officers; 121 Enlisted
Price:2billion
*MUNITIONS*
AIR-LAUNCHED
AIM-7 SPARROW
http://www.globalsecurity.org/military/systems/munitions/images/aim-7-dvic402-s.jpgPrimary Function Air-to-air guided missile
Contractor Raytheon Co.
Power Plant Hercules MK-58 solid-propellant rocket motor
Thrust Classified
Speed Classified
Range approximately 30 nm
Length 12 feet (3.64 meters)
Diameter 8 inches (0.20 meters)
Wingspan 3 feet, 4 inches (1 meter)
Warhead Annular blast fragmentation warhead
88 lbs high explosive for AIM-9H
Launch Weight Approximately 500 pounds (225 kilograms)
Guidance System Raytheon semiactive on either continuous wave or pulsed Doppler radar energy
Date Deployed 1976
Aircraft Platforms Navy: F-14 and F/A-18;
Air Force: F-4, F-15, and F-16;
Marine Corps: F-4 and F/A-18
Unit Cost Approximately $125,000
AGM-119B PENGUIN ANTI- SHIP MISSILE
http://www.globalsecurity.org/military/systems/munitions/images/agm-119-980721-n-5961c-001-s.jpg
Primary Function Helicopter launched anti-ship missile.
Contractor Kongsberg Vaapenfabrikk (Norway)
Power Plant Solid propellant rocket motor and solid propellant booster
Length 120.48 inches (3.06 meters)
Launch Weight 847 pounds (385 kilograms)
Diameter 11.2 inches (28.45 centimeters)
Wing Span 30 in's folded, 55 in's Deployed
Range 25 nautical miles / 35 km
Speed 1.2 Mach maximum
Guidance Inertial and infrared terminal.
Warhead 265 lbs gross, 110 lbs High Explosive, semi armor piercing
derivative of the Bullpup missile
Date Deployed Fourth quarter 1993
Price: 100,000
AGM-65 MAVERICK
http://www.globalsecurity.org/military/systems/munitions/images/agm-65-dvic443-s.jpg
Primary Function: Air-to-surface guided missile Contractors: Hughes Aircraft Co., Raytheon Co. Power Plant: Thiokol TX-481 solid-propellant rocket motor Autopilot Proportional Navigation Stabilizer Wings/Flippers Propulsion Boost Sustain Variant AGM-65A/B AGM-65D AGM-65G AGM-65E AGM-65F Service Air Force Marine Corps Navy Launch Weight: 462 lbs
(207.90 kg) 485 lbs
(218.25 kg) 670 lbs
(301.50 kg) 630 lbs
(286 kg) 670 lbs
(301.50 kg) Diameter: 1 foot (30.48 centimeters) Wingspan: 2 feet, 4 inches (71.12 centimeters) Range: 17+ miles (12 nautical miles/27 km) Speed: 1150 km/h Guidance System: electro-optical television imaging infrared Laser infrared homing Warhead: 125 pounds
(56.25 kilograms)
cone shaped 300 pounds
(135 kilograms)
delayed-fuse penetrator, heavyweight 125 pounds
(56.25 kilograms)
cone shaped 300 pounds
(135 kilograms)
delayed-fuse penetrator, heavyweight Explosive 86 lbs. Comp B 80 lbs. PBX(AF)-108 Fuse Contact FMU-135/B COSTS Air Force
AGM-65D/G Navy
AGM-65E/F
Price: 122,230
SUBMARINE LAUNCHED
BGM-109 TOMAHAWK
http://www.globalsecurity.org/military/systems/munitions/images/slcm-dvic469-s.jpg
Primary Function: Long-range subsonic cruise missile for attacking land targets.
Contractor: Raytheon Co. [ex Hughes Missile Systems Co.] Tucson, Ariz.
Power Plant: Williams International F107-WR-402 cruise turbo-fan engine; solid-fuel booster
Length: 18 feet 3 inches (5.56 meters); with booster: 20 feet 6 inches (6.25 meters)
Weight: 2,650 pounds (1192.5 kg); 3,200 pounds (1440 kg) with booster
Diameter: 20.4 inches (51.81 cm)
Wing Span: 8 feet 9 inches (2.67 meters)
Range: Land attack, conventional warhead: 600 nautical miles (690 statute miles, 1104 km)
Speed: Subsonic - about 550 mph (880 km/h)
Guidance System: Inertial and TERCOM
Warheads: Conventional: 1,000 pounds Bullpup, or Conventional submunitions dispenser with combined effect bomblets, or WDU-36 warhead w/ PBXN-107 explosive & FMU-148 fuze, or 200 kt. W-80 nuclear device
Date Deployed: 1983
Cost $100,000
AGM-84 HARPOON/SLAM
http://www.globalsecurity.org/military/systems/munitions/images/harpoon-13-s.jpg
Primary Function: Air-to-surface anti-ship missile Mission Maritime ship attack Targets Maritime surface Service Navy and Air Force Contractor: Boeing [ex McDonnell Douglas] Power Plant: Teledyne Turbojet and solid propellant booster for surface and submarine launch Program status Operational sea-launch air-launch SLAM SLAM-ER First capability 1977 1979 Thrust: 660 pounds Length: 15 feet
(4.55 meters) 12 feet, 7 inches
(3.79 meters) 14 feet, 8 inches
(4.49 meters) Weight: 1,470 pounds
(661.5 kilograms) 1,145 pounds
(515.25 kilograms) 1,385 pounds
(629.55 kilograms) Diameter: 13.5 inches (34.29 centimeters) Wingspan: 3 feet (91.44 centimeters) Range: Greater than 60 nautical miles 150+ miles Speed: 855 km/h Guidance System: Sea-skimming cruise with mid-course guidance monitored by radar altimeter, active seeker radar terminal homing inertial navigation system with GPS, infrared terminal guidance Warheads: Penetration high-explosive blast (488 pounds) Explosive Destex Fuze Contact Quantity Navy: 5,983; Air Force: 90 Platforms A-6 <../aircraft/a-6.htm>, F/A-18 <../aircraft/f-18.htm>, S-3 <../aircraft/s-3.htm>, P-3 <../aircraft/p-3.htm>, B-52H, ships
Price: 474,609
*NUCLEAR DEVICES* terms of agreement.
1. the nation of bringerofpain shall not be held in anyway responsible for the actions of other nations.
2. the nation of bringerofpain has the right to ignore an order.
3. By buying these nuclear devices, you are agreeing that you are
a) 1 month or older
b) are not in anyway a, warmongerer,newbie,godmodder.
4. you will not, in anyway, use these weapons against bringerofpain, my allies, and or occupied states.
B61-3/4/10
description- non-strategic bomb.
Yield- 0.3 to 350
delivery system- f-15,f-16,f-18, NATO tornado
primary use- air to surface
price: 300million
B61-7/11
description- strategic bomb
yield- 10 to 350
delivery system- b52, b-2
primary use- air to surface
price:500million
W62
description- ICBM warhead
yield- 170
delivery system- minuteman III ICBM
primary use- surface to surface
price- 400million
B83
description- strategic bomb
yield- low to 1,200
delivery system- B-52,B-2
primary use-air to surface
Price: 550million
GROUND SYSTEMS
M60 PATTON
http://www.globalsecurity.org/military/systems/ground/images/m-60a1-dvic351-s.jpg
Weight 60 tons Length 32'4" Width 13'6" Height 12'6" Ground Clearance 18in Track Width 28in Forward speed 30 mph Reverse speed 10 mph Engine 750 hp Continental AVDS-1790 V-12 diesel Vertical obstacle climb 49 in Maximum width ditch 108 in Fording Depth 48 in Main Gun 105mm/51cal M68 rifiled gun with 63 rounds Coaxial machinegun M240 - 7.62mm with 5,950 rounds Commander's machinegun M85 - .50 cal antiaircraft gun with 900 rounds Sensors and Fire Control M21 solid state along ballistic computer, AN/VVG-2 ruby laser rangefinder usable by both commander and gunner, AN/vsg-2 Tank thermal Sights (TTS) withlaser rangerfinder and Mercury-Cadmium-Telluride (HgCdTe) IR detector for passive night and dust vision.
price:2million
M113 ARMED PERSONNEL CARRIER
http://www.globalsecurity.org/military/systems/ground/images/m113-001-s.jpg
Length 191.5" Width 105.75" Height 86.5" Clearance 16" Weight, combat loaded 27,180 lb. (12,329 kg) Maximum weight 31,000 lb. (14,061 kg) Net weight 23,880 lb. (10,832 kg) Air drop weight 22,128 lb. (10,037 kg) Personnel capacity 2 + 11 Fuel tank capacity 95 gallons (360 liters) Ground pressure 8.63 psi (0.60 kg/cm2)
Performance
Speed on land 41 mi/h (66 km/h) Speed in water, with track 3.6 mi/h (5.8 km/h) Cruising range 300 mi (483 km) Turning radius Pivot to infinite Slope 60% Side slope 40% Trench crossing 66 in. (168 cm) Vertical wall climbing 24 in. (61 cm) Braking (20-0 mi/h) 40 ft.
Engine
Make and model Detroit Diesel 6V53T Displacement 318 in.3 (5.2 liter) Fuel Diesel (DF2) Rated horsepower 275 hp Gross horsepower-to-weight ratio 20.2 hp/ton
Transmission, Automatic
Make and model Allison X200-4B Type Hydrokinetic Steering Hydrostatic Brake type Multiple wet plate
Running Gear
Suspension Torsion bar Road wheels 5 per side, 24 inch diameter (61 cm) Track type Steel single pin, detachable rubber pad Number of shoes 63 left, 64 right Track pitch 6 in. (15.2 cm) Track width 15 in. (38 cm) Shock absorbers 3 per side Wheel travel 9.0 in. (22.9 cm)
Electrical System
Generator Amperes 200, 300 optional Volts, dc 28 Batteries 4, type 6TL, 120 amp-hr, 12-volt each
Armament
50 cal MG 2,000 ready rds.
Armor
Basic hull 5083 Aluminum Bolt-on armor kit Steel armor Mine armor Steel armor Gun shield kit Steel armor Spall suppressant Composite panel
Fire Extinguishers
Fixed 5 lb. (2.3 kg) CO2 for engine compartment Portable 5 lb. (2.3 kg) CO2
price:3million
XM104 WOLVERINE( heavy assault bridge system)
http://www.globalsecurity.org/military/systems/ground/images/wol3-s.jpg
http://www.globalsecurity.org/military/systems/ground/images/wolverine2-s.jpg
Crew 2 Soldiers (12B MOS) Weight 68.7 TONS Powerpack AGT-1500 Turbine X1100 Trans Launch Power Unit Integrated APU Powers Launcher Silent Watch Fire Protection Automatic 3 Zone Extinguisher System Electrical System 24 Volts Tread 112.0 in. Track Width 25.0 in. Vertical Obstacle 36.7 in. Trench Crossing 106 in. Ground Clearance 19.0 in. Fording 48 in. (w/o kit) Speed Cross Country: 32.2 kph Improved Roads: 56 kph Maximum:45 MPH (Governed) Cruising Range 260 Miles Heavy Assault Bridge System Gap Crossing Length 24.0 M (26 Meter Length) Mission Load Class [MLC] 70.0 TONS Crossing Speed 13-16 kph Durability 5000 MLC70 Crossings Launch Time Less than 5 min. Recovery Time 10 Minutes (5 Min. to Engage, 5 Min to store in Travel Mode
price: 3.5million
M55 8" SELF PROPELLED HOWITZER(T108)
http://www.globalsecurity.org/military/systems/ground/images/m55-img17-s.jpg
M55: General Manufacturer Pacific Car and Foundry Co. . M55: Dimensions Combat weight 98,000lbs / 44,000kg Length without howitzer 311" / 790cm Height 140"360cm Width Howitzer overhang forward 0" . M55: Armament Type 8" Howitzer M47 Mount T58 in turret Ammunition 10 rounds Traverse 60° (30° left or right) Elevation +65° to -5° rate of fire one round every two minutes maximum range 16,900 meters Type .50cal M2HB MG Mount Flexible in turret AA mount Ammunition Traverse 360° (manual) Elevation Manual . M55: Armor Assembly Welding Maximum .59"1.5cm Hull Rolled homogeneous steel Turret Rolled homogeneous steel . M55: Automotive Engine Continental AV-1790-5B; 12 cylinder, 4 cycle, 90° vee gasoline Horsepower Gross: 810@2800rpm Transmission Allison CD-850-4A, two ranges forward, 1 reverse Steering Wobble stick Brakes Multiple disc . M55: Suspension Type Torsion bar Road wheels 7 independently sprung dual/track Track return rollers 3 dual/track Drive sprockets 11-tooth front drive Idlers Rear road wheels serve as adjustable trailing idlers M55: Track Type T84E1 Center guide, double pin, chevron, rubber Width 23"58cm Pitch 6"15cm . M55: Performance Max level road speed 32mph51kph Max grade 0.6 Min turning diameter Pivot Cruising range ~160mi, roads~260km, roads Max trench 90"230cm Max vertical obstacle 40"100cm Max fording depth 48"120cm
price: 3million
* AIR UNITS*
T-28 TALON
http://www.globalsecurity.org/military/systems/aircraft/images/t-38-199905172ship-s.jpg
Primary Function Advanced jet pilot trainer
Builder Northrop Corp.
Power Plant Two General Electric J85-GE-5 turbojet engines with afterburners
Thrust 2,900 pounds (1,315 kilograms) with afterburners
Length 46 feet, 4 1/2 inches (14 meters)
Height 12 feet, 10 1/2 inches (3.8 meters)
Wingspan 25 feet, 3 inches (7.6 meters)
Speed 812 mph (Mach 1.08 at sea level)
Ceiling Above 55,000 feet (16,667 meters)
Maximum Takeoff Weight 12,500 pounds (5,670 kilograms)
Range 1,000 miles (870 nautical miles)
Armament T-38A: none; AT-38B has provisions for external armament
Unit Cost $756,000
F-14 TOMCAT
http://www.globalsecurity.org/military/systems/aircraft/images/f-14-dvic222-s.jpg
Function Carrier-based multi-role strike fighter
Contractor Grumman Aerospace Corporation
Propulsion F-14: two Pratt & Whitney TF-30P-414A
turbofan engines with afterburners;
F-14B and F-14D: two General Electric F-110-GE-400
augmented turbofan engines with afterburners
Thrust F-14A: 20,900 pounds (9,405 kg) static thrust per engine;
F-14B and F-14D: 27,000 pounds (12,150 kg) per engine Length 61 feet 9 inches (18.6 meters) Height 16 feet (4.8 meters) Basic Weight approx 43,600 pounds Maximum Takeoff Weight 72,900 pounds (32,805 kg) Wingspan 64 feet (19 meters) unswept,
38 feet (11.4 meters) swept Reference wing area 565 sq ft. Wing aspect ratio 7.28 Ceiling Above 53,000 feet Max G 6.5 Speed 1,584 mph (2,548km/h) Max. speed at 40,000 ft (12,200 m)
Max Mach Number = 1.88
Cruise Mach Number = .72
Carrier Approach Speed = 125 kts Fuel 16, 200 lbs. Internal fuel
3, 800 lbs. External fuel Maximum range 1,600 nm (2,573km) Mission Radius 500 nm (930 km) Hi-Med-Hi strike profile
380 nm (700 km) Hi-Lo-Lo-Hi strike profile Airfield 2,500 ft. Field takeoff distance
2,400 ft. Field landing distance Crew Two: pilot and radar intercept officer
Armament Up to 13,000 pounds of
Air-to-Air Missiles (up to)
6 AIM-7 Sparrows <../munitions/aim-7.htm>
4 AIM-9 Sidewinder <../munitions/aim-9.htm>
6 AIM-54 Phoenix <../munitions/aim-54.htm>
air-to-ground ordnance
MK-82 <../munitions/mk82.htm> (500 lbs.)
4 MK-83 <../munitions/mk83.htm>(1,000 lbs.)
4 MK-84 <../munitions/mk84.htm> (2,000 lbs.)
MK-20 <../munitions/mk20.htm> cluster bomb
4 GBU-10 <../munitions/gbu-10.htm> LGB
GBU-12 MK-82 <../munitions/gbu-12.htm>LGB
4 GBU-16 MK-83 <../munitions/gbu-16.htm>LGB
4 GBU-24 MK-84 <../munitions/gbu-24.htm>LGB
4 GBU-31 <../munitions/gbu-31.htm> JDAM <../munitions/jdam.htm>(2,000 lbs)
one MK-61A1 Vulcan 20mm cannon
Selected F-14A and B are wired to carry TARPS <../../../../irp/program/collect/tarps.htm>
All F-14D's are wired to carry the TARPS <../../../../irp/program/collect/tarps.htm>
Countermeasures AN/ALR-45 radar warning receiver [Itek] AN/ALR-67 radar warning receiver [F-14D] AN/ALQ-167 ECM Pod [F-14D] AN/ALE-50 towed decoy [F-14D] Date Deployed First flight: December 21st 1970 Inventory 157 F-14A/B
53 F-14D
Phasing out one squadron / year
All to be withdrawn by 2010
F-14 orginally designed for 6,000 flight hours
Currently certified for 7,350 flight hours
Potential for extension to 8,000 or 9,000 flight hours
Price:38 million
FH-1 PHANTOM
First flight Jan. 26, 1945
Wingspan 40 feet 9 inches (wings folded, 16 feet, 3 inches)
Length 38 feet 9 inches
Height 14 feet, 2 inches
Weight 10,035 lbs
Speed 500 mph (max.)
Ceiling 41,100 ft
Range 695 miles
Accommodation One crew
Armament Four 22 mm cannons
Power plant Two 1,600-pound thrust Westinghouse J30-WE-20 turbojets
Price:12million
F-16XL FIGHTING FALCON
http://www.globalsecurity.org/military/systems/aircraft/images/f-16-eglin1-s.jpg
Crew size F-16XL-2 two-seat cockpit
F-16XL-1 single-seat aircraft
Length 54.2 ft (16.52 m)
Wingspan 34.3 ft (10.45 m)
height at vertical tail 17.7 ft (5.39 m).
Max. weight 48,000 lb (17,915.60 kg)
Engines F-16XL-2 General Electric F110-GE-129 engine (with afterburner) rated at 29,000 lb thrust.
F-16XL-1 Pratt and Whitney 100-PW-100 engine (with afterburner), rated at 23,830 lb thrust.
Controls Both aircraft featured an analog fly-by-wire electronic flight control system during the laminar flow research. The single-seat aircraft now has a digital flight control system.
Wing construction The delta (cranked arrow) wings on both aircraft are manufactured of advanced graphite composites to provide strength for high wing loads during flight.
Design load Baseline F-16XL: 9 "Gs".
Modified F-16XL: 3 "Gs")
Maximum Speed F-16XL-2, Mach 2 (approx. 1,400 mph) (2,253 k/hr)
F-16XL-1, Mach 1.8 (approx. 1,260 mph)
Range Over 2,500 nautical miles (4,630 k), without in-flight refueling, and unlimited with in-flight refueling
Price: 40 million
F-22 RAPTOR
http://www.globalsecurity.org/military/systems/aircraft/images/f-22-9733679-s.jpg
Official Nickname Raptor
User U. S. Air Force
Function Air superiority fighter
Contractors Lockheed Martin Aeronautical Systems: F-22 program management, the integrated forebody (nose section) and forward fuselage (including the cockpit and inlets), leading edges of the wings, the fins and stabilators, flaps, ailerons, landing gear and final assembly of the aircraft.
Lockheed Martin Tactical Aircraft Systems: Center fuselage, stores management, integrated navigation and electronic warfare systems (INEWS), the communications, navigation, and identification (CNI) system, and the weapon support system.
Boeing: wings, aft fuselage (including the structures necessary for engine and nozzle installation), radar system development and testing, avionics integration, the training system, and flight-test development and management.
Pratt & Whitney: F119-PW-100 engines that power the Raptor.
Major Subcontractors Approximately 240 firms in 37 states are considered major subcontractors
More than 1,150 firms in 46 states and Puerto Rico, along with firms in seven international countries make up the F-22/F119 subcontractor team.
(partial list):
Northrop Grumman
Texas Instruments
Kidde-Graviner Ltd.
Allied-Signal Aerospace
Hughes Radar Systems
Harris
Fairchild Defense
GEC Avionics
Lockheed Sanders
Kaiser Electronics
Digital Equipment Corp.
Rosemount Aerospace
Curtiss-Wright Flight Systems
Dowty Decoto, EDO Corp.
Lear Astronics Corp.
Parker-Hannifin Corp.
Simmonds Precision
Sterer Engineering
TRW
XAR
Motorola
Hamilton Standard
Sanders/GE Joint Venture
Menasco Aerospace
Projected Employment 15,000 in EMD and 27,000 in production
Propulsion two Pratt & Whitney F119-PW-100 engines
Thrust 35,000 lbst
Length 62.08 feet, 18.90 meters
Height 16.67 feet, 5.08 meters
Wingspan 44.5 feet, 13.56 meters
Wing Area 840 square feet
Horizontal Tailspan 29 feet, 8.84 meters
Maximum Takeoff Weight
Ceiling
Speed Mach 1.8 (supercruise: Mach 1.5)
Crew one pilot
Armament Two AIM-9 Sidewinders
six AIM-120C Advanced Medium-Range Air-to-Air Missiles (AMRAAM)
one 20mm Gatling gun
two 1,000-pound Joint Direct Attack Munitions (JDAM)
First flight: September 7, 1997
Flight Test Aircraft: Nine
Flight Test Program Length 1997 until 2003 (Approximately 2,700 flights covering roughly 4,800 test hours in EMD)
Price: 45million
B-52 STRATOFORTRESS( note, if you are less than a month old, you will be sold the ones without nuclear capability.)
http://www.globalsecurity.org/wmd/systems/images/b52-bomb-s.jpg
Primary Function: Heavy bomber
Contractor: Boeing Military Airplane Co.
Power Plant: Eight Pratt & Whitney engines TF33-P-3/103 turbofan
Thrust: Each engine up to 17,000 pounds (7,650 kilograms)
Length: 159 feet, 4 inches (48.5 meters)
Height: 40 feet, 8 inches (12.4 meters)
Wingspan: 185 feet (56.4 meters)
Speed: 650 miles per hour (Mach 0.86)
Ceiling: 50,000 feet (15,151.5 meters)
Weight: Approximately 185,000 pounds empty (83,250 kilograms)
Maximum Takeoff Weight: 488,000 pounds (219,600 kilograms)
Range: Unrefueled 8,800 miles (7,652 nautical miles)
Armament:
NOTE: The B-52 can carry 27 internal weapons. Authoritative sources diverge as to maximum munition loads, with some suggesting as many as 51 smaller munitions and 30 larger munitions, while others suggest maximum loads of 45 and 24, respectively.
The Heavy Stores Adaptor Beam [HSAB] external pylon can carry only 9 weapons which limits the total carry to 45 (18 external).
The AGM-28 pylon could carry lighter weapons like the MK-82 and can carry 12 weapons on each pylon, for a total of 24 external weapons, for a the total of 51. However, the AGM-28 pylon is no longer used, so the B-52 currently carries on HSABs, limiting the external load to 18 bombs, or a total of 45 bombs.
Approximately 70,000 pounds (31,500 kilograms) mixed ordnance -- bombs, mines and missiles.
NUCLEAR
20 ALCM
12 SRAM [ext]
12 ACM [ext]
2 B53 [int]
8 B-61 Mod11 [int]
8 B-83 [int]
CONVENTIONAL
51 CBU-52 (27 int, 18 ext)
51 CBU-58 (27 int, 18 ext)
51 CBU-71 (27 int, 18 ext)
30 CBU 87 (6 int, 18 ext)
30 CBU 89 (6 int, 18 ext)
30 CBU 97 (6 int, 18 ext)
51 M117
18 Mk 20 (ext)
51 Mk 36
8 Mk 41
12 Mk 52
8 Mk 55
8 Mk 56
51 Mk 59
8 Mk 60 (CapTor)
51 Mk. 62
8 Mk. 64
8 Mk 65
51 MK 82
18 MK 84 (ext)
PRECISION
18 JDAM (12 ext)
30 WCMD (16 ext)
8 AGM-84 Harpoon
20 AGM-86C CALCM
8 AGM-142 Popeye [3 ext]
18 AGM-154 JSOW (12 ext)
12 AGM-158 JASSSM [ext]
12 TSSAM
Systems AN/ALQ-117 PAVE MINT active countermeasures set
AN/ALQ-122 false target generator [Motorola]
AN/ALQ-153 tail warning set [Northrop Grumman]
AN/ALQ-155 jammer Power Management System [Northrop Grumman]
AN/ALQ-172(V)2 electronic countermeasures system [ITT]
AN/ALR-20A Panoramic countermeasures radar warning receiver
AN/ALR-46 digital warning receiver [Litton]
AN/ALT-32 noise jammer
12 AN/ALE-20 infra-red flare dispensers
6 AN/ALE-24 chaff dispensers
AN/ANS-136 Inertial Navigation Set
AN/APN-224 Radar Altimeter
AN/ASN-134 Heading Reference
AN/APQ-156 Strategic Radar
AN/ASQ-175 Control Display Set
AN/AYK-17 Digital Data Display
AN/AYQ-10 Ballistics Computer
AN/AAQ-6 FLIR Electro-optical viewing system
AN/AVQ-22 Low-light TV Electro-optical viewing system
AN/ARC-210 VHF/UHF communications
AN/ARC-310 HF radio communications
CRM-114 Discriminator
Crew: Five (aircraft commander, pilot, radar navigator, navigator and electronic warfare officer)
Accommodations: Six ejection seats
Unit Cost: $30 million
B-1B LANCER
http://www.globalsecurity.org/wmd/systems/images/b1_cbus-s.jpg
Primary Function: Long-range, multi-role, heavy bomber
Builder: Rockwell International, North American Aircraft
Operations Air Frame and Integration: Offensive avionics, Boeing Military Airplane; defensive avionics, AIL Division
Power Plant: Four General Electric F-101-GE-102 turbofan engine with afterburner
Thrust: 30,000-plus pounds (13,500-plus kilograms) with afterburner, per engine
Length: 146 feet (44.5 meters)
Wingspan: 137 feet (41.8 meters) extended forward,
79 feet (24.1 meters) swept aft
Height: 34 feet (10.4 meters)
Weight: Empty, approximately 190,000 pounds (86,183 kilograms)
Maximum Takeoff Weight: 477,000 pounds (214,650 kilograms)
Speed: 600+ mph (Mach .92) @ 500 feet
825 mph (Mach 1.25) @ 50,000 feet
Rotate and Takeoff Speeds: 210 Gross - 119 Rotate kts / 134 kts Takeoff
390 Gross - 168 kts Rotate / 183 kts Takeoff
Landing Speeds: 210 Gross - 145 kts
380 Gross - 195 kts
Range: 7,455 miles, unrefueled
3,444 miles with normal weapons load
Ceiling: 60,000 feet (18,000 meters)
Crew: Four (aircraft commander, pilot, offensive systems officer and defensive systems officer)
Armament: NUCLEAR
CONVENTIONAL
84 Mk 62
84 MK82
30 CBU 87
30 CBU 89
30 CBU 97
12 Mk 65
PRECISION
30 WCMD
24 JDAM
12 GBU-27
12 AGM-154 JSOW
12 TSSAM
Date Deployed: June 1985
Cost: $200 million
B-2 SPIRIT (note, if you are under a month old, have enough money, and wish to purchase one of these, you will recieve the plane without nuclear capabilities)
http://www.globalsecurity.org/wmd/systems/images/b2bombs_s.jpg
http://www.globalsecurity.org/wmd/systems/images/b-2-clouds-s.jpg
Primary function: Multi-role heavy bomber.
Prime Contractor: Northrop Grumman Corp.
Contractor Team: Boeing Military Airplanes Co.,
General Electric Aircraft Engine Group
Hughes Training Inc., Link Division
Power Plant/Manufacturer: Four General Electric F-118-GE-100 engines
Thrust: 17,300 pounds each engine (7,847 kilograms)
Length: 69 feet (20.9 meters)
Height: 17 feet (5.1 meters)
Wingspan: 172 feet (52.12 meters)
Speed: High subsonic
Ceiling: 50,000 feet (15,152 meters)
Takeoff Weight (Typical): 336,500 pounds (152,635 kilograms)
Range: Intercontinental, unrefueled
Armament: NUCLEAR
16 B61
16 B83
16 AGM-129 ACM
16 AGM-131 SRAM 2 CONVENTIONAL
80 MK82 [500lb]
16 MK84 [2000lb]
34-36 CBU87
34-36 CBU89
34-36 CBU97
PRECISION
80 GBU-30 JDAM [500lb]
16 GBU-32 JDAM [2000lb]
8 GBU 27
8 EGBU 28
8 GBU 36
8 GBU 37
8-16 AGM-154 JSOW
8-16 AGM-137 TSSAM
Payload: 40,000 pounds (18,000 kilograms)
Crew: Two pilots
Unit cost: Approximately $2.1 billion [average]
AH-64 APACHE
http://www.globalsecurity.org/military/systems/aircraft/images/apache_hellfire-s.jpg
http://www.globalsecurity.org/military/systems/aircraft/images/ah-64-dvic292-s.jpg
Contractors Boeing McDonnell Douglas Helicopter Systems(Mesa, AZ)
General Electric (Lynn, MA)
Martin Marietta (Orlando, FL) Propulsion Two T700-GE-701Cs Crew Two AH-64A AH-64D Length 58.17 ft (17.73 m) 58.17 ft (17.73 m) Height 15.24 ft (4.64 m) 13.30 ft (4.05 m) Wing Span 17.15 ft (5.227 m) 17.15 ft (5.227 m) Primary Mission Gross Weight 15,075 lb (6838 kg)
11,800 pounds Empty 16,027 lb (7270 kg) Lot 1 Weight Hover In-Ground Effect (MRP) 15,895 ft (4845 m)
[Standard Day]
14,845 ft (4525 m)
[Hot Day ISA + 15C] 14,650 ft (4465 m)
[Standard Day]
13,350 ft (4068 m)
[Hot Day ISA + 15 C] Hover Out-of-Ground Effect (MRP) 12,685 ft (3866 m)
[Sea Level Standard Day]
11,215 ft (3418 m)
[Hot Day 2000 ft 70 F (21 C)] 10,520 ft (3206 m)
[Standard Day]
9,050 ft (2759 m)
[Hot Day ISA + 15 C] Vertical Rate of Climb (MRP) 2,175 fpm (663 mpm)
[Sea Level Standard Day]
2,050 fpm (625 mpm)
[Hot Day 2000 ft 70 F (21 C)] 1,775 fpm (541 mpm)
[Sea Level Standard Day]
1,595 fpm (486 mpm)
[Hot Day 2000 ft 70 F (21 C)] Maximum Rate of Climb (IRP) 2,915 fpm (889 mpm)
[Sea Level Standard Day]
2,890 fpm (881 mpm)
[Hot Day 2000 ft 70 F (21 C)] 2,635 fpm (803 mpm)
[Sea Level Standard Day]
2,600 fpm (793 mpm)
[Hot Day 2000 ft 70 F (21 C)] Maximum Level Flight Speed 150 kt (279 kph)
[Sea Level Standard Day]
153 kt (284 kph)
[Hot Day 2000 ft 70 F (21 C)] 147 kt (273 kph)
[Sea Level Standard Day]
149 kt (276 kph)
[Hot Day 2000 ft 70 F (21 C)] Cruise Speed (MCP) 150 kt (279 kph)
[Sea Level Standard Day]
153 kt (284 kph)
[Hot Day 2000 ft 70 F (21 C)] 147 kt (273 kph)
[Sea Level Standard Day]
149 kt (276 kph)
[Hot Day 2000 ft 70 F (21 C)] Range 400 km - internal fuel
1,900 km - internal and external fuel Armament M230 30mm Gun <systems/m230.htm>
70mm (2.75 inch) Hydra-70 Folding-Fin Aerial Rockets <../munitions/hydra-70.htm>
AGM-114 Hellfire <../munitions/agm-114.htm> anti-tank missiles
AGM-122 Sidearm <../munitions/agm-122.htm>anti-radar missile
AIM-9 Sidewinder <../munitions/aim-9.htm>Air-to-Air missiles
<images/ah-64d-mission-image20.jpg> <images/ah-64d-mission-image20.jpg>Mission Equipment Target Acquisition and Designation System /
Pilot Night Vision System Reliability The general objective of aircraft readiness is to achieve 75% Mission Capable.
price:15million
*NAVAL*
BB-61 IOWA-CLASS BATTLESHIP
http://www.globalsecurity.org/military/systems/ship/images/bb-62-8406362-s.jpg
http://www.globalsecurity.org/military/systems/ship/images/missour2-s.jpg
Displacement Light Displacement: 45231 tons
Full Displacement: 57271 tons
Dead Weight: 12040 tons
Length Overall Length: 888 ft
Waterline Length: 860 ft
Beam Extreme Beam: 109 ft
Waterline Beam: 108 ft
Draft Maximum Navigational Draft: 38 ft
Draft Limit: 37 ft
Max Speed 35 knots
Power Plant Eight boilers, four geared turbines, four shafts, 212,000 shaft horsepower
Armament 32 - Tomahawk ASM/LAM - 8 armored box launchers
16 - Harpoon ASM - 4 quad cell launchers
9 - Mk 7 - 16-inch / 50 caliber guns
12 - Mk 28 - 5-inch / 38 caliber guns
4 - Mk 15 - 20mm Phalanx CIWS
Combat Systems SPS-49 Air Search Radar
SPS-67 Surface Search Radar
4 Mk37 Gun Fire Control
2 Mk38 Gun Direction
1 Mk40 Gun Director
1 SPQ-9
SLQ-25 NIXIE
SLQ-32 EW system
Aircraft None embarked
landing area and unhangared parking area
4 SH-3 or
4 SH-60
Compliment 1,515 ship's company
65 officers
1,450 enlisted
58 Marines
Builders New York Navy Yard -- BB 61, 63
Philadelphia Navy Yard -- BB 62, 64
Price: 3billion
[b]CVN-68 NIMITZ-CLASS
http://www.globalsecurity.org/military/systems/ship/images/vinson-bow-s.jpg
Builder Newport News Shipbuilding Co., Newport News, Va.
Power Plant Two Nuclear Power Plant (A4W Pressurized Water Reactor)
Four shafts, Four propellers, with five blades each
Length, overall 1,092 feet (332.85 meters)
Flight Deck Width 252 feet (76.8 meters)
Beam 134 feet (40.84 meters)
Displacement Approx. 97,000 tons (87,300 metric tons) full load
Speed 30+ knots (34.5+ miles per hour)
Aircraft 85
Aircraft elevators Four
Catapults Four
Armament 4 Sea Sparrow launchers
3 Phalanx CIWS 20mm mounts [Nimitz & Ike]
4 Phalanx CIWS 20mm mounts [Vinson and later]
Combat Systems SPS-48E 3-D air search radar
SPS-49(V)5 2-D air search radar
3 Mk91 Fire Control
Multi-Function Radar (MFR) [CVN-77]
Volume Search Radar (VSR) [CVN-77]
AN/SLQ-32(V)4 active jamming/deception
AN/WLR-1H ESM
Service Life 50 years
Crew Ship's Company: 3,200
Air Wing: 2,480
Departments
Administrative
Aircraft Maintenance
Air
Chaplain
Combat Systems
Deck
Dental
Engineering
Legal
Maintenance
Medical
Navigation
Operations
Public Affairs
Reactor
Safety
Supply
Training
Weapons
Price: 4billion
ohio-class SSBN ( note, if you are under 1 month old, you shall be sold the non-nuclear subs)
http://www.globalsecurity.org/wmd/systems/images/ssbn_uw_s.jpg
http://www.globalsecurity.org/wmd/systems/images/ssbn731-p01a_s.jpg
Builders: General Dynamics Electric Boat Division.
Power Plant: One S8G nuclear reactor
core reloaded every nine years
two geared steam turbines,
one shaft, output of 60,000 hp
Length: 560 feet (170.69 meters)
Beam: 42 feet (10.06 meters)
Displacement: Surfaced: 16,764 tons
Submerged:18,750 tons
Speed: Official: 20+ knots (23+ miles per hour, 36.8 +kph)
Actual: 25 knots submerged speed
Operating Depth: Official: "greater than 800 feet"
Actual: greater than 1,000 feet
Armament: 24 - tubes for Trident I and II,
4 - torpedo tubes with Mk48 Torpedoes
Systems: AN/BQQ-6 passive-only spherical bow and conformal sonar arrays
AN/BQR-19 active short range navigation set
AN/BQS-13 Active sonar
AN/BQS-15 high-frequency short range under-ice sonar set
TB-16B or TB-23 passive towed array
AN/BPS-15A I-Band search and navigation radar
AN/WLR-8(V) radar receiver
MK 98 Digital Missile Fire Control System (FCS) for Trident missiles
MK 118 Torpedo FCS
Crew: 15 Officers, 140 Enlisted
Price:500million
SSN-21 SEAWOLF CLASS SUB
http://www.globalsecurity.org/military/systems/ship/images/ssn-21-dvic117-s.jpg
Builders General Dynamics Electric Boat Division
Power Plant One S6W reactor
one shaft at with 52,000 shp with pumpjet propulsor
Improved Performance Machinery Program Phase II one secondary propulsion submerged motor
Length 353 feet (107.6 meters)
Draft 35 feet (10.67 meters)
Beam 40 feet (12.2 meters)
Displacement 7,460 ton surface displacement
9,137 tons submerged displacement
Speed Official: 25+ knots (28+ miles per hour, 46.3+ kph)
Actual: 35 knots maximum submerged speed
Actual: 20 knots tactical ["silent"] speed
Operating Depth Official: "greater than 800 feet"
Actual: About 1600 feet
Jane's Fighting Ships: 2000 feet
Armament eight 660-mm torpedo tubes
50 Tomahawk cruise missiles or
50 Harpoon antiship missiles or
50 Mark 48 ADCAP torpedoes or
up to 100 mines
Systems AN/BSY-2 active-passive Sonar/Fire Control w/
hemispherical bow array and wide aperture array
TB-16B or TB-23 towed array
AN/BPS-16 search and navigation radar
AN/WLQ-4(V)1 ES receiver
Central Combat System (CCS) MK2
Link 11 Tactical data link
OTCIXS Tactical data link
Crew 12 Officers; 121 Enlisted
Price:2billion
*MUNITIONS*
AIR-LAUNCHED
AIM-7 SPARROW
http://www.globalsecurity.org/military/systems/munitions/images/aim-7-dvic402-s.jpgPrimary Function Air-to-air guided missile
Contractor Raytheon Co.
Power Plant Hercules MK-58 solid-propellant rocket motor
Thrust Classified
Speed Classified
Range approximately 30 nm
Length 12 feet (3.64 meters)
Diameter 8 inches (0.20 meters)
Wingspan 3 feet, 4 inches (1 meter)
Warhead Annular blast fragmentation warhead
88 lbs high explosive for AIM-9H
Launch Weight Approximately 500 pounds (225 kilograms)
Guidance System Raytheon semiactive on either continuous wave or pulsed Doppler radar energy
Date Deployed 1976
Aircraft Platforms Navy: F-14 and F/A-18;
Air Force: F-4, F-15, and F-16;
Marine Corps: F-4 and F/A-18
Unit Cost Approximately $125,000
AGM-119B PENGUIN ANTI- SHIP MISSILE
http://www.globalsecurity.org/military/systems/munitions/images/agm-119-980721-n-5961c-001-s.jpg
Primary Function Helicopter launched anti-ship missile.
Contractor Kongsberg Vaapenfabrikk (Norway)
Power Plant Solid propellant rocket motor and solid propellant booster
Length 120.48 inches (3.06 meters)
Launch Weight 847 pounds (385 kilograms)
Diameter 11.2 inches (28.45 centimeters)
Wing Span 30 in's folded, 55 in's Deployed
Range 25 nautical miles / 35 km
Speed 1.2 Mach maximum
Guidance Inertial and infrared terminal.
Warhead 265 lbs gross, 110 lbs High Explosive, semi armor piercing
derivative of the Bullpup missile
Date Deployed Fourth quarter 1993
Price: 100,000
AGM-65 MAVERICK
http://www.globalsecurity.org/military/systems/munitions/images/agm-65-dvic443-s.jpg
Primary Function: Air-to-surface guided missile Contractors: Hughes Aircraft Co., Raytheon Co. Power Plant: Thiokol TX-481 solid-propellant rocket motor Autopilot Proportional Navigation Stabilizer Wings/Flippers Propulsion Boost Sustain Variant AGM-65A/B AGM-65D AGM-65G AGM-65E AGM-65F Service Air Force Marine Corps Navy Launch Weight: 462 lbs
(207.90 kg) 485 lbs
(218.25 kg) 670 lbs
(301.50 kg) 630 lbs
(286 kg) 670 lbs
(301.50 kg) Diameter: 1 foot (30.48 centimeters) Wingspan: 2 feet, 4 inches (71.12 centimeters) Range: 17+ miles (12 nautical miles/27 km) Speed: 1150 km/h Guidance System: electro-optical television imaging infrared Laser infrared homing Warhead: 125 pounds
(56.25 kilograms)
cone shaped 300 pounds
(135 kilograms)
delayed-fuse penetrator, heavyweight 125 pounds
(56.25 kilograms)
cone shaped 300 pounds
(135 kilograms)
delayed-fuse penetrator, heavyweight Explosive 86 lbs. Comp B 80 lbs. PBX(AF)-108 Fuse Contact FMU-135/B COSTS Air Force
AGM-65D/G Navy
AGM-65E/F
Price: 122,230
SUBMARINE LAUNCHED
BGM-109 TOMAHAWK
http://www.globalsecurity.org/military/systems/munitions/images/slcm-dvic469-s.jpg
Primary Function: Long-range subsonic cruise missile for attacking land targets.
Contractor: Raytheon Co. [ex Hughes Missile Systems Co.] Tucson, Ariz.
Power Plant: Williams International F107-WR-402 cruise turbo-fan engine; solid-fuel booster
Length: 18 feet 3 inches (5.56 meters); with booster: 20 feet 6 inches (6.25 meters)
Weight: 2,650 pounds (1192.5 kg); 3,200 pounds (1440 kg) with booster
Diameter: 20.4 inches (51.81 cm)
Wing Span: 8 feet 9 inches (2.67 meters)
Range: Land attack, conventional warhead: 600 nautical miles (690 statute miles, 1104 km)
Speed: Subsonic - about 550 mph (880 km/h)
Guidance System: Inertial and TERCOM
Warheads: Conventional: 1,000 pounds Bullpup, or Conventional submunitions dispenser with combined effect bomblets, or WDU-36 warhead w/ PBXN-107 explosive & FMU-148 fuze, or 200 kt. W-80 nuclear device
Date Deployed: 1983
Cost $100,000
AGM-84 HARPOON/SLAM
http://www.globalsecurity.org/military/systems/munitions/images/harpoon-13-s.jpg
Primary Function: Air-to-surface anti-ship missile Mission Maritime ship attack Targets Maritime surface Service Navy and Air Force Contractor: Boeing [ex McDonnell Douglas] Power Plant: Teledyne Turbojet and solid propellant booster for surface and submarine launch Program status Operational sea-launch air-launch SLAM SLAM-ER First capability 1977 1979 Thrust: 660 pounds Length: 15 feet
(4.55 meters) 12 feet, 7 inches
(3.79 meters) 14 feet, 8 inches
(4.49 meters) Weight: 1,470 pounds
(661.5 kilograms) 1,145 pounds
(515.25 kilograms) 1,385 pounds
(629.55 kilograms) Diameter: 13.5 inches (34.29 centimeters) Wingspan: 3 feet (91.44 centimeters) Range: Greater than 60 nautical miles 150+ miles Speed: 855 km/h Guidance System: Sea-skimming cruise with mid-course guidance monitored by radar altimeter, active seeker radar terminal homing inertial navigation system with GPS, infrared terminal guidance Warheads: Penetration high-explosive blast (488 pounds) Explosive Destex Fuze Contact Quantity Navy: 5,983; Air Force: 90 Platforms A-6 <../aircraft/a-6.htm>, F/A-18 <../aircraft/f-18.htm>, S-3 <../aircraft/s-3.htm>, P-3 <../aircraft/p-3.htm>, B-52H, ships
Price: 474,609
*NUCLEAR DEVICES* terms of agreement.
1. the nation of bringerofpain shall not be held in anyway responsible for the actions of other nations.
2. the nation of bringerofpain has the right to ignore an order.
3. By buying these nuclear devices, you are agreeing that you are
a) 1 month or older
b) are not in anyway a, warmongerer,newbie,godmodder.
4. you will not, in anyway, use these weapons against bringerofpain, my allies, and or occupied states.
B61-3/4/10
description- non-strategic bomb.
Yield- 0.3 to 350
delivery system- f-15,f-16,f-18, NATO tornado
primary use- air to surface
price: 300million
B61-7/11
description- strategic bomb
yield- 10 to 350
delivery system- b52, b-2
primary use- air to surface
price:500million
W62
description- ICBM warhead
yield- 170
delivery system- minuteman III ICBM
primary use- surface to surface
price- 400million
B83
description- strategic bomb
yield- low to 1,200
delivery system- B-52,B-2
primary use-air to surface
Price: 550million